Functional Analysis Approach to Minimum Energy Maneuver Problem for Flexible Space Structures-Reference-Cited by-同舟云学术

Functional Analysis Approach to Minimum Energy Maneuver Problem for Flexible Space Structures

Published:2002-11 Issue:6 Volume:25 Page:1136-1142
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Fujii Hironori A.¹,Suda Shin-ichi¹

Affiliation:

1. Tokyo Metropolitan Institute of Technology, Tokyo 191-0065, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.4993

Reference13 articles.

1. Closed-loop soft-constrained time-optimal control of flexible space structures

2. Time-optimal slewing of flexible spacecraft

3. Comparison between robustified feedforward and feedback for achieving parameter robustness

4. Robust time-optimal control - Frequency domain approach

5. Fuel/time optimal control of the benchmark problem

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Bending and torsional vibration attenuation of multi-panel deployable solar array using reaction wheel actuators;Aircraft Engineering and Aerospace Technology;2022-07-08

2. Maneuver Motion Planning Based on Virtual Target for UAVs;Lecture Notes in Electrical Engineering;2021-10-30

3. Vibration reduction of flexible solar array during orbital maneuver;Aircraft Engineering and Aerospace Technology;2014-02-25

4. Turn over Problem of Tether Satellite System;56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law;2005-10-17

5. Slew Maneuver of a Flexible Space Structure with Constraint on Bending Moment;Journal of Guidance, Control, and Dynamics;2003-03